AIR INTAKE OF AN AIRCRAFT NACELLE INCLUDING A REINFORCED LIP WITH A JOULE EFFECT DE-ICING SYSTEM

AIR INTAKE OF AN AIRCRAFT NACELLE INCLUDING A REINFORCED LIP WITH A JOULE EFFECT DE-ICING SYSTEM

The intake (40) has a first alveolar structure (60.1) that is made of a material for conducting the heat, where the heat is flattened against an inside surface of a wall (52) and provided between the wall and a defrosting system (58). A second alveolar structure (60.2) is made of composite material...

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Bibliographische Detailangaben
Hauptverfasser: PORTE, ALAIN, CHELIN, FRÉDÉRIC
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:The intake (40) has a first alveolar structure (60.1) that is made of a material for conducting the heat, where the heat is flattened against an inside surface of a wall (52) and provided between the wall and a defrosting system (58). A second alveolar structure (60.2) is made of composite material that is adjacent to the first alveolar structure, where the second alveolar structure is flattened against the inside surface of the wall, with the defrosting system and inserted between the second alveolar structure and the wall. The alveolar structures are made of aluminum alloy. An independent claim is also included for an aircraft nacelle.